Commonwealth legislation

AD/PC-6/17 - Landing Gear Strut - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Pilatus PC‑6 aeroplanes with serial numbers before 570 to have the landing‑gear strut physically modified in accordance with Pilatus Service Bulletin No. 35, completed by 2 November 1967. The directive sets the obligation, method reference and deadline but gives no rationale, cost allocation or enforcement details.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/PC-6/17 - Landing Gear Strut - Modification.

AD/PC-6/17 - Landing Gear Strut - Modification

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Pilatus Porter PC-6 Series Aeroplanes

AD/PC-6/17 Landing Gear Strut - Modification N/K

Applicability: All models prior to S/No. 570. Document: Pilatus SB No. 35.

Compliance: Before 2 November 1967.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.